CN102030103B - 飞行器的第一限制值指示器失效时的辅助驾驶方法和装置 - Google Patents
飞行器的第一限制值指示器失效时的辅助驾驶方法和装置 Download PDFInfo
- Publication number
- CN102030103B CN102030103B CN2010102980735A CN201010298073A CN102030103B CN 102030103 B CN102030103 B CN 102030103B CN 2010102980735 A CN2010102980735 A CN 2010102980735A CN 201010298073 A CN201010298073 A CN 201010298073A CN 102030103 B CN102030103 B CN 102030103B
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- driving
- auxiliary driving
- engine
- limits value
- engines
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- Expired - Fee Related
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- 238000000034 method Methods 0.000 title claims abstract description 31
- 238000012544 monitoring process Methods 0.000 claims abstract description 53
- 230000008569 process Effects 0.000 claims description 12
- 230000015556 catabolic process Effects 0.000 abstract description 4
- 239000007789 gas Substances 0.000 description 13
- 238000004519 manufacturing process Methods 0.000 description 10
- 230000008676 import Effects 0.000 description 7
- 230000001105 regulatory effect Effects 0.000 description 7
- 230000009183 running Effects 0.000 description 4
- 238000013459 approach Methods 0.000 description 3
- 238000006731 degradation reaction Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 230000009467 reduction Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000004093 laser heating Methods 0.000 description 1
- 230000002045 lasting effect Effects 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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- 230000000737 periodic effect Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Feedback Control In General (AREA)
- Testing Of Engines (AREA)
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Toys (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0904541 | 2009-09-23 | ||
FR09/04541 | 2009-09-23 | ||
FR0904541A FR2950324B1 (fr) | 2009-09-23 | 2009-09-23 | Procede et dispositif d'aide au pilotage d'un aeronef en cas de pannes d'un indicateur de premiere limitation |
Publications (2)
Publication Number | Publication Date |
---|---|
CN102030103A CN102030103A (zh) | 2011-04-27 |
CN102030103B true CN102030103B (zh) | 2013-11-13 |
Family
ID=42111813
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2010102980735A Expired - Fee Related CN102030103B (zh) | 2009-09-23 | 2010-09-21 | 飞行器的第一限制值指示器失效时的辅助驾驶方法和装置 |
Country Status (4)
Country | Link |
---|---|
US (1) | US8412388B2 (fr) |
EP (1) | EP2301844B1 (fr) |
CN (1) | CN102030103B (fr) |
FR (1) | FR2950324B1 (fr) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2973340B1 (fr) * | 2011-03-30 | 2013-04-12 | Eurocopter France | Procede, dispositif d'aide au pilotage d'un aeronef, et aeronef |
FR2973840B1 (fr) * | 2011-04-07 | 2015-09-18 | Airbus Operations Sas | Procede et dispositif pour la commande du regime des moteurs d'un aeronef au cours d'une phase de decollage. |
FR2976395B1 (fr) * | 2011-06-10 | 2013-08-02 | Eurocopter France | Systeme d'aide au pilotage et aeronef. |
FR2989796B1 (fr) | 2012-04-20 | 2014-04-11 | Eurocopter France | Instrument de secours pour aeronef combinant des informations de vol, une information de marge de puissance et une assistance au pilotage |
FR3015574B1 (fr) * | 2013-12-20 | 2019-05-03 | Safran Helicopter Engines | Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif |
FR3020658B1 (fr) * | 2014-04-30 | 2020-05-15 | Safran Aircraft Engines | Capot de recuperation d'huile de lubrification pour un equipement de turbomachine |
WO2017055975A1 (fr) * | 2015-09-30 | 2017-04-06 | Bombardier Inc. | Procédé et système pour la présentation d'un état de fonctionnement d'un moteur d'aéronef |
US10099796B2 (en) * | 2016-10-04 | 2018-10-16 | General Electric Company | System and method for dynamically controlling the operation of an aircraft |
US10683099B2 (en) * | 2017-02-08 | 2020-06-16 | Pratt & Whitney Canada Corp. | Methods and systems for controlling operation of aircraft engines |
CN108803643B (zh) * | 2018-06-19 | 2021-08-20 | 成都纵横自动化技术股份有限公司 | 飞行控制方法、装置、飞行控制器及复合翼飞行器 |
FR3090576B1 (fr) * | 2018-12-20 | 2021-09-10 | Airbus Helicopters | Procédé d’assistance pour aéronef monomoteur à voilure tournante lors d’une panne moteur. |
FR3107511B1 (fr) | 2020-02-20 | 2022-01-21 | Airbus Helicopters | Dispositif de surveillance d’une marge de poussée pour giravion, giravion associé et procédé correspondant |
FR3134564B1 (fr) | 2022-04-15 | 2024-07-19 | Airbus Helicopters | Procédé et système d'aide au pilotage d'un aéronef, aéronef équipé d’un tel système. |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4794755A (en) * | 1987-05-14 | 1989-01-03 | The United States Of America As Represented By The Secretary Of The Air Force | Back-up control system for F101 engine and its derivatives |
EP0816226A1 (fr) * | 1996-06-07 | 1998-01-07 | Eurocopter | Indicateur de pilotage pour aéronef |
US5986580A (en) * | 1997-12-22 | 1999-11-16 | Eurocopter | Flight control indicator for aircraft |
US6150959A (en) * | 1998-05-18 | 2000-11-21 | Eurocopter | System for monitoring the operation of an aircraft, especially a helicopter |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2680386B1 (fr) * | 1991-08-12 | 1993-11-05 | Aerospatiale Ste Nationale Indle | Dispositif pour la commande du regime des moteurs d'un aeronef. |
GB2272783B (en) * | 1992-11-20 | 1996-05-22 | Rolls Royce Plc | Aircraft engine control system |
US6568166B2 (en) * | 2000-12-22 | 2003-05-27 | Pratt & Whitney Canada Corp. | Back-up control apparatus for turbo machine |
US7212942B2 (en) * | 2003-06-10 | 2007-05-01 | Precision Innovations Llc | Power available and limitation indicator for use with an aircraft engine |
US7043896B2 (en) * | 2003-11-21 | 2006-05-16 | Pratt & Whitney Canada Corp. | Method and apparatus for controlling fuel flow to an engine |
ITTO20040050A1 (it) * | 2004-02-03 | 2004-05-03 | Agusta Spa | Dispositivo indicatore di un margine di potenza residua di motori a turbina di velivoli |
FR2871520B1 (fr) * | 2004-06-15 | 2008-12-26 | Eurocopter France | Indicateur de pilotage permettant de predire l'evolution des parametres de surveillance d'un turbomoteur |
US7075457B1 (en) * | 2004-09-22 | 2006-07-11 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration (Nasa) | Energy index for aircraft maneuvers |
FR2878288B1 (fr) * | 2004-11-25 | 2007-01-19 | Eurocopter France | Procede et dispositif pour optimiser l'enveloppe de performances d'un turbomoteur |
US7414544B2 (en) * | 2005-01-28 | 2008-08-19 | Bell Helicopter Textron, Inc. | Power situation indicator |
FR2902408B1 (fr) * | 2006-06-19 | 2008-08-08 | Eurocopter France | Equilibrage en puissance de deux turbomoteurs d'un aeronef |
-
2009
- 2009-09-23 FR FR0904541A patent/FR2950324B1/fr not_active Expired - Fee Related
-
2010
- 2010-07-22 EP EP10007617A patent/EP2301844B1/fr active Active
- 2010-09-16 US US12/883,738 patent/US8412388B2/en active Active
- 2010-09-21 CN CN2010102980735A patent/CN102030103B/zh not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4794755A (en) * | 1987-05-14 | 1989-01-03 | The United States Of America As Represented By The Secretary Of The Air Force | Back-up control system for F101 engine and its derivatives |
EP0816226A1 (fr) * | 1996-06-07 | 1998-01-07 | Eurocopter | Indicateur de pilotage pour aéronef |
US5986580A (en) * | 1997-12-22 | 1999-11-16 | Eurocopter | Flight control indicator for aircraft |
US6150959A (en) * | 1998-05-18 | 2000-11-21 | Eurocopter | System for monitoring the operation of an aircraft, especially a helicopter |
Also Published As
Publication number | Publication date |
---|---|
US20110071708A1 (en) | 2011-03-24 |
FR2950324A1 (fr) | 2011-03-25 |
EP2301844A1 (fr) | 2011-03-30 |
CN102030103A (zh) | 2011-04-27 |
EP2301844B1 (fr) | 2012-11-21 |
US8412388B2 (en) | 2013-04-02 |
FR2950324B1 (fr) | 2011-08-26 |
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Owner name: AIRBUS HELICOPTER Free format text: FORMER NAME: ULOCOPT S.A. |
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CP01 | Change in the name or title of a patent holder |
Address after: France, Anna Patentee after: Kong Kezhishengji Address before: France, Anna Patentee before: EUROCOPTER |
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CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131113 |
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CF01 | Termination of patent right due to non-payment of annual fee |